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US20180088004A1 - Fuel system smart node - Google Patents

Fuel system smart node
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Publication number
US20180088004A1
US20180088004A1US15/557,953US201615557953AUS2018088004A1US 20180088004 A1US20180088004 A1US 20180088004A1US 201615557953 AUS201615557953 AUS 201615557953AUS 2018088004 A1US2018088004 A1US 2018088004A1
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US
United States
Prior art keywords
engine
sensors
fuel
sensor data
flow
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US15/557,953
Inventor
Patrick W. Kalgren
Brian Drost
Kenneth Gravenstede
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sikorsky Aircraft Corp
Original Assignee
Sikorsky Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sikorsky Aircraft CorpfiledCriticalSikorsky Aircraft Corp
Priority to US15/557,953priorityCriticalpatent/US20180088004A1/en
Assigned to SIKORSKY AIRCRAFT CORPORATIONreassignmentSIKORSKY AIRCRAFT CORPORATIONASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS).Assignors: GRAVENSTEDE, Kenneth, DROST, BRIAN, KALGREN, PATRICK W.
Publication of US20180088004A1publicationCriticalpatent/US20180088004A1/en
Abandonedlegal-statusCriticalCurrent

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Abstract

A measuring system, method, and/or computer program that realizes physics-based relations between sensor readings to monitor for degradations and predict failures of power systems is provided. For example, the supply and return of fuel in a power system is provided by a fuel injection system. The fuel injection system responds to changes in loads and system conditions, such as to compensate for fuel loss due to fuel combustion, by continuously and instantaneously changing the fuel flow. This behavior by the fuel injection system creates characteristic signatures. These characteristic signatures are instantaneously detected and utilized by the measuring system, method, and/or computer program to detect healthy, degrading, failing, and failed mechanical conditions so as to monitor for degradations and predict failures of the power system.

Description

Claims (12)

US15/557,9532015-03-172016-01-13Fuel system smart nodeAbandonedUS20180088004A1 (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
US15/557,953US20180088004A1 (en)2015-03-172016-01-13Fuel system smart node

Applications Claiming Priority (3)

Application NumberPriority DateFiling DateTitle
US201562134353P2015-03-172015-03-17
PCT/US2016/013152WO2016164091A1 (en)2015-03-172016-01-13Fuel system smart node
US15/557,953US20180088004A1 (en)2015-03-172016-01-13Fuel system smart node

Publications (1)

Publication NumberPublication Date
US20180088004A1true US20180088004A1 (en)2018-03-29

Family

ID=57072158

Family Applications (1)

Application NumberTitlePriority DateFiling Date
US15/557,953AbandonedUS20180088004A1 (en)2015-03-172016-01-13Fuel system smart node

Country Status (2)

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US (1)US20180088004A1 (en)
WO (1)WO2016164091A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN111927623A (en)*2020-06-222020-11-13北京航空航天大学 High-altitude ventilation and dynamic performance simulation test platform for two-stroke aviation piston engine
CN113374577A (en)*2021-06-272021-09-10华能太原东山燃机热电有限责任公司Bus type gas supply pipeline state monitoring system for gas generator set

Citations (5)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US4464895A (en)*1982-05-261984-08-14Chandler Evans Inc.Gas turbine engine starting technique and control
US5052174A (en)*1988-07-281991-10-01Williams International CorporationContinuous flow fuel control system
US5103636A (en)*1988-07-281992-04-14Williams International CorporationContinuous flow fuel control system
US5205161A (en)*1990-12-141993-04-27Erwin Curtis LFuel consumption measurement system
US6209309B1 (en)*1997-12-192001-04-03Hamilton Sundstrand CorporationPulse width modulated fuel flow control for an engine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US6553290B1 (en)*2000-02-092003-04-22Oshkosh Truck CorporationEquipment service vehicle having on-board diagnostic system
US6941785B2 (en)*2003-05-132005-09-13Ut-Battelle, LlcElectric fuel pump condition monitor system using electrical signature analysis

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US4464895A (en)*1982-05-261984-08-14Chandler Evans Inc.Gas turbine engine starting technique and control
US5052174A (en)*1988-07-281991-10-01Williams International CorporationContinuous flow fuel control system
US5103636A (en)*1988-07-281992-04-14Williams International CorporationContinuous flow fuel control system
US5205161A (en)*1990-12-141993-04-27Erwin Curtis LFuel consumption measurement system
US6209309B1 (en)*1997-12-192001-04-03Hamilton Sundstrand CorporationPulse width modulated fuel flow control for an engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN111927623A (en)*2020-06-222020-11-13北京航空航天大学 High-altitude ventilation and dynamic performance simulation test platform for two-stroke aviation piston engine
CN113374577A (en)*2021-06-272021-09-10华能太原东山燃机热电有限责任公司Bus type gas supply pipeline state monitoring system for gas generator set

Also Published As

Publication numberPublication date
WO2016164091A1 (en)2016-10-13

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Owner name:SIKORSKY AIRCRAFT CORPORATION, CONNECTICUT

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